Presentation is loading. Please wait.

Presentation is loading. Please wait.

STRENGTH OF MATERIALS(1)

Similar presentations


Presentation on theme: "STRENGTH OF MATERIALS(1)"— Presentation transcript:

1 STRENGTH OF MATERIALS(1)
MINISTORY OF SCIENCE AND TECHNOLOGY DEPARTMENT OF TECHNICAL AND VOCATIONAL EDUCATION STRENGTH OF MATERIALS(1) A.G.T.I (Second Year) Prof. U Kyaw San Department of Mechanical Engineering. Y.T.U

2 Load, Stress and Strain, Hook’s law ,
Scope of Presentation Chapter 1 Direct Stress Load, Stress and Strain, Hook’s law , Principal of Superposition & Example Problems Tensile Test , Factor of Safety Strain Energy, Resilience & Example Problems Impact Loads & Example Problems Varying Cross-section and Loads & Example Problems Strain Energy , Resilience & Example Problems Compound Bars & Example Problems Temperature Stresses & Example Problems

3 Chapter 2 Shear stress Shear Stress Shear Strain Modulus of Rigidity
Shear Strain Energy Example Problems

4 Chapter 1 1.1 Load Typical loading types are Static load or dead load ,ie non-fluctuating load, generally caused by gravity effects. Live load as produced by, for example lorries crossing a bridge Impact or shock load caused by sudden blows Fatigue, Fluctuating or alternating loads, the magnitude and sign of the load changing with time The simplest type of load is Direct push or pull , known as tension or compression Units newton (N) , kilonewton (kN) , meganewton (MN)

5 P 1.2 Stress force ( pull) Tensile stress = Cross-sectional area P tensile force P force ( push) Compression stress = Cross-sectional area compression force P

6 2.3 Strain Bar in tension P l x P l x

7 Example 2 ( Page-11 in ME 2014) P x l Given data
Tensile load P = 15,000 kg Steel rod diameter, d = 2 cm To find stress Calculation - 7 -

8 Example 4 ( Page 12 in ME 2014 ) P x l Given data
A wire , Tensile strain  = Elongation x = mm To find Length of wire l Calculation

9 1.4 Hook’s law, Principal of superposition
stress ( load)  strain (extension) L x P Strain ( elongation) Stress (load) Stress – strain graph Substituting  = P / L and  = x / L Principal of superposition The effect of a system of forces acting on a body is equal to the sum of the effects these same forces applied.

10 Example 5 ( Page-12 ~13 in ME 2014 ) A B 100 C 5 m y PCA PCB 50 x x
Given data two steel rods Length l = 5 m Working stress  = 560 kg/cm2 E = 2.1 x 106 kg/cm2 A B C 5 m x 10 tonnes 100 P = 10 x1000 kg 50 PCA PCB x y To find Diameter of rod d = ? Elongation x =? Calculation Fx = 0 gives PCA = PCB Fy = 0 gives 10,000 kg = 2 x PCA cos 50 PCA = kgs

11 Example 6 ( Page-14 ~15 in ME 2014 ) B C D 10000 lb 9000 lb 2000 lb
2 ft 3 ft 4 ft 1 2 3 Given data A steel bar cross-sectional area = 1 in2 forces are shown in figure E = 30 x 106 lb/in2 1 2 3 10000 lb (applied) 9000 lb B C 3000 lb 2000 lb Action from 1 , lb 9000 lb ( action from 3 ) 7000 lb ,Resultant Resultant 7000 lb To find The stresses in each portion = ? total elongation = ? Similarly CD = 9000 lb / in2 ,xCD = in Total elongation = xAB + XBC + xCD = in - 11 -

12 1.3 Tensile Test Universal tensile testing machine
Specimen and extensometer

13 A – Proportional limit B – Elastic limit C – Upper yield point
D – Lower yield point E – Ultimate limit F - Fracture point

14 Example 7 ( Page-24 in ME 2014 ) Given data A tensile test result
a mild steel specimen d = 2 cm gauge length l = 4 cm At the limit of proportionality, PA = N the extension , xA = mm Yield load, PC = N The maximum load PE = N After bring broken , gauge length l’ =5,56 cm at the neck, dia. d’ = 1.58 cm To find Young ‘s modulus = E =? The stress at the proportionality = ? The yield stress = ? Ultimate stress = ? Percentage elongation and contraction =? Solution Cross-sectional area A = /4 X 22 = cm2

15 Example 8 ( Page-26 in ME 2014 ) 60 tonnes compression load Given data
I cm Wall thickness 60 tonnes compression load A short hollow Cast iron cylinder Given data P= 60 tonnes ultimate crushing stress = 5400 kg/cm2 factor of safety = 3 P To find Outside diameter , D = ? Calculation P 1 cm , thickness d d = D - 2 D - 15 -

16 1.10 Impact loads ( Page-30 in ME 2014 )
h x W Area, A Weight = W Falling height = h Maximum instantaneous tensile stress = I Equivalent load = P Maximum instantaneous extension = x Assuming the stress induced does not exceed the elastic limit Loss of potential energy of weight = Gain of strain energy of rod = Strain energy stored in rod W ( h +x ) = ½ x Pi X where x = i L / E Pi = I A Induced tensile stress in the rod Where W in N , h & L in mm , A in mm2 and E in N/mm2 - 16 -

17 Example 11 ( Page-34 in ME 2014 ) =  x 102 mm2 1 = 132.92 N/mm2
Given data W = 100 kg = 9.81 x 100 N d = 2 cm = 20 mm L = 3 m = 3000 mm h = 4 cm = 40 mm E = 205,000 N/mm2 L h x W Area, A To find Maximum stress set up I = ? Solution A =  (d/2)2 =  x 102 mm2 1 = N/mm2 - 17 -

18 1.11 Varying cross-section and loads
P L1 L2 L3 d1 d2 d3 1 2 3 Loads P = P1 = P2 = P3 P = 1 A1 = 2 A2 = 3 A3 The changes in length The total changes of length = x1 + x x3 - 18 -

19 Example 12 ( Page-36 in ME 2014 ) 3 1 2 P= 10000 lb P d2=1in
Given data A wrought iron bar d1 = 1 1/8 in L1 = 6 ft = 6 x 12 in d2 = 1 in L2 = 12 ft = 12 x 12 in d3 = 1 ¼ in L3 = ( 24 – 6 – 12 ) = 6 ft = 6 x 12 in E = 28 x 106 lb/in2 P = 10,000 lb 1 2 P= lb d1 =1 1/8 in d2=1in P d3=1 ¼ in L1= 6ft L3= 6 ft L2= 12ft Solution To find The total change in length =? The energy stored in the bar =? - 19 -

20 1.11 Compound bars ( Page 37 in ME-2014)
Rod A Tube B LA = LB Rigid two plates Equilibrium equation P = PA PB …… (1) P = A AA + B AB Compatibility equation (strain equation) xA = xB ….. (2) A LA =  B LB A = B - 20 -

21 Example 13 ( Page 39 in ME 2014) Concrete column P = 100 tons
Given data Concrete column 18 x 18 in. square 4 steel rods d = 1 in. EC = 2 x 106 lb/in2 ,ES = 30 x 106 lb/in2 Load P = 100 tons = 100 x 2240 lbs P = 100 tons Concrete column 4 steel rods d = 1 in A Section A -A 18 in To find S = ? , C = ? Solution Area of steel rod , AS = 4 x (/4) x d2 = 3.14 in2 Net area of concrete AC = 18 x 18 – 3.14 = in2 For compound bar P = S AS + C AC = S x C x eq.(1) From equations (1) and (2), C = 608 lb/in2 , S = 9120 lb/in2 (Ans) - 21 -

22 1.12 Temperature stresses ( P-41 in ME- 2014 )
Brass Steel L B L t S L t Extension of steel. XS Compression of brass, xB Final position of Compound bar Original position of Free expansion due to temp. rise. t For compound bar Subjected to a change of temperature t Let B = compressive stress induced in the bar due to rise in trmp. T xB = compression of bar dur to trmp. change Similarly Strain equation XT = S L T xS for steel rod xT = S L T - xS for copper cube xS + X B = L T (B - C ) XT Equilibrium equation PS = PB S AS = B AB -22 -

23 Example 15 ( Page-45 in ME 2014 ) S2 =5391.99 kg/cm2 (Tensile)
Given data A steel rod dS = 25 mm A brass tube external dia. DB = 35 mm internal dia. dB = 25 mm Induced stress in steel due to tighten initially S = 100 kg/cm2 Temperature rise t = 60C To find The final stresses in the rod and the tube Solution Induced stress in steel due to tighten initially S1 = 100 kg/cm2 , tension ( given) Equilibrium equation S1 AS = B1 AB where AS = /4 x = 4.91 cm and AB = /4 ( ) = 4.71 cm2 100 x = B x 4.71 B1 = kg/ cm2 , compression From equation (1) & (2) S2 = kg/cm2 (Tensile) B2 = kg/cm2 ( comp) Due to rise in temperature t = 60 C Equilibrium equation P = S2 x AS = B2 x AB S2 x = B2 x eq(1) Final stresses S= S1+S2= kg/cm2 ( tensile) B= B1+B2= kg/cm2 (compressive) Strain equation - 23 -

24 CHAPTER 2 Shear Stress L M 2.2 Shear strain Ø 2.3 Modulus of rigidity
2.4 Shear strain energy Strain energy ( U) = Work done in straining = ½ ( final couple ) x ( Angle turned through U =(2/2 G ) x volume - 24 -

25 Example 2 ( Page-36 in ME 2014 ) P Given data
1.4 cm d=10 cm P Weight support shaft collar Given data A solid circular shaft and collar The ultimate shear stress = 3 tonnes / cm2 Factor of safety N = 3 To find The greatest compressive load P =? Tthe maximum stress on the shaft = ? Solution Shearing area in collar Acollar =  d t =  x 10 x 1.4 cm2 - 25 -

26 Example 3 ( Page-57 in ME 2014 ) T Circle dia. d = 14 cm Coupling bolt
shaft Power 250 kW, 1000 rpm P P P P P P T Given data Transmit power P =250 kW rpm = 1000 No of bolts n = 6 Pitch circular dia = 14 cm Allowable shear stress bolt =75 N/cm2 To find diameter of bolt = ? - 26 -

27 Example 6 ( Page-62 in ME 2014 ) Given data Key width = 1.25 cm W
A shaft diameter = 4 cm A key width = 1.25 cm length = 5 cm Allowable shear stress key = 650 kg/cm2 Lever arm distance = 1 m Key width = 1.25 cm W P d To find Applied force W = ? 4 cm diameter shaft 1 m Solution Key shearing area A = width x key length A key = x 5 cm2 - 27 -

28 Example 7 ( Page-65 in ME 2014 ) Given data diameter of rod d = 5 cm
Thickness of cotter = 1.25 cm Permissible stress tension stress T = 300 N/mm2 shear stress in member mem = 150 N/mm2 shear stress in cotter cot = 225 N/mm2 crushing stress  = 450 N/mm2 To find Required diameters in the joint shown Solution P = 300 N/mm2 x (  / 4 ) x 502 = N eq (1) Shear of cotter 225 = 588,000 / ( 2 e x 12.5 ) e = 105 mm eq(2) Crushing between right-hand member and cotter 450 = 588,000 / ( 2 a x 12.5 ) a = 52.4 mm eq(5) Shear of right –hand member 150 = 588,000 / 4 ab Ab = 980 mm eq(3) From equation(3) b = mm Crushing between left-hand member and cotter 450 = 558,000 / ( 12.5 x h ) h = mm From equation(4) C = 18.7 mm Shear of left–hand member 150 = 588,000 / 2 ch Ch = 1960 mm eq(4) - 28-

29 THANK YOU VERY MUCH


Download ppt "STRENGTH OF MATERIALS(1)"

Similar presentations


Ads by Google